压缩机的蒸发冷却

M. S. Dzitoev, Y. Tatarenko, А.V. Моlоsтоv
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引用次数: 0

摘要

本文讨论了用向气体中注入液体的方法冷却容积式压缩机工作流体的前景。本文介绍了利用KOMDET - VKA软件对某直线驱动往复式压缩机级在不同压比下的运行情况进行数值分析的结果。对于蒸发冷却,建议使用氮气、氦气和氩气混合的空气。这些试剂用于太空火箭的供气系统。在往复式压缩机中,通过向工作物质的吸入腔中注入液体来实现蒸发冷却的便利性。它可以减少压缩工作量和注气温度,并提高其生产率。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
On evaporative cooling of compressor
The paper considers the perspectives of cooling the working fluid in a volumetric compressor by injecting liquid into gas. The results of numerical analysis for the operation of the stage of a linear‑driven reciprocating compressor using KOMDET‑VKA software at different pressure ratios in the stage are presented. For evaporative cooling, it is proposed to use a mixture of air with nitrogen, helium, and argon. These agents are used in the gas supply systems of space rockets. The expediency of using evaporative cooling by injecting liquid into the suction cavity of the working substance in a reciprocating compressor is shown. It allows reducing the compression work and gas injection temperature as well as increasing increase its productivity.
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